Based on the primary principle of flight dynamics, the paper studies the flight quality of Tailless Flying-wing HALE UAV and Taill Flying-wing according to traditional calculation methods.

• 本论文以经典飞行动力学原理为基础，利用传统的飞行力学计算分析方法，对飞翼布局的高空长航时无人机的飞行品质与有尾飞翼布局和常规布局的飞行品质进行了对比研究。